WO2009056287A1 - Feuille de matériau et procédé pour sa préparation - Google Patents

Feuille de matériau et procédé pour sa préparation Download PDF

Info

Publication number
WO2009056287A1
WO2009056287A1 PCT/EP2008/009122 EP2008009122W WO2009056287A1 WO 2009056287 A1 WO2009056287 A1 WO 2009056287A1 EP 2008009122 W EP2008009122 W EP 2008009122W WO 2009056287 A1 WO2009056287 A1 WO 2009056287A1
Authority
WO
WIPO (PCT)
Prior art keywords
tapes
material sheet
tape
woven fabric
sheet according
Prior art date
Application number
PCT/EP2008/009122
Other languages
English (en)
Inventor
Reinard Jozef Maria Steeman
Marcel Jongedijk
Johann Van Elburg
Shaban Hoxha
José MEZA-CUADRA
Original Assignee
Dsm Ip Assets B.V.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dsm Ip Assets B.V. filed Critical Dsm Ip Assets B.V.
Priority to US12/740,475 priority Critical patent/US20110174147A1/en
Priority to EP20080829955 priority patent/EP2205927B1/fr
Priority to KR1020167002867A priority patent/KR101647940B1/ko
Priority to AU2008317960A priority patent/AU2008317960B2/en
Priority to CN200880114233.7A priority patent/CN101842658B/zh
Publication of WO2009056287A1 publication Critical patent/WO2009056287A1/fr
Priority to IL204659A priority patent/IL204659A/en
Priority to US14/977,046 priority patent/US20160107344A1/en
Priority to US16/248,668 priority patent/US10632652B2/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/003—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor characterised by the choice of material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C55/00—Shaping by stretching, e.g. drawing through a die; Apparatus therefor
    • B29C55/02—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets
    • B29C55/04—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets uniaxial, e.g. oblique
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/18—Layered products comprising a layer of metal comprising iron or steel
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/32—Layered products comprising a layer of synthetic resin comprising polyolefins
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/022—Non-woven fabric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/028—Net structure, e.g. spaced apart filaments bonded at the crossing points
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
    • B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B9/041—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B9/047—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material made of fibres or filaments
    • D—TEXTILES; PAPER
    • D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02G—CRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G3/00—Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
    • D02G3/02—Yarns or threads characterised by the material or by the materials from which they are made
    • D02G3/06—Threads formed from strip material other than paper
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00—Woven fabrics designed to make specified articles
    • D03D1/0035—Protective fabrics
    • D03D1/0052—Antiballistic fabrics
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/20—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads
    • D03D15/283—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads synthetic polymer-based, e.g. polyamide or polyester fibres
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/30—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the structure of the fibres or filaments
    • D03D15/37—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the structure of the fibres or filaments with specific cross-section or surface shape
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/40—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the structure of the yarns or threads
    • D03D15/44—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the structure of the yarns or threads with specific cross-section or surface shape
    • D03D15/46—Flat yarns, e.g. tapes or films
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/50—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the properties of the yarns or threads
    • D03D15/573—Tensile strength
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
    • D03D15/50—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the properties of the yarns or threads
    • D03D15/587—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the properties of the yarns or threads adhesive; fusible
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00—Armour; Armour plates
    • F41H5/02—Plate construction
    • F41H5/04—Plate construction composed of more than one layer
    • F41H5/0414—Layered armour containing ceramic material
    • F41H5/0428—Ceramic layers in combination with additional layers made of fibres, fabrics or plastics
    • F41H5/0435—Ceramic layers in combination with additional layers made of fibres, fabrics or plastics the additional layers being only fibre- or fabric-reinforced layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00—Armour; Armour plates
    • F41H5/02—Plate construction
    • F41H5/04—Plate construction composed of more than one layer
    • F41H5/0442—Layered armour containing metal
    • F41H5/0457—Metal layers in combination with additional layers made of fibres, fabrics or plastics
    • F41H5/0464—Metal layers in combination with additional layers made of fibres, fabrics or plastics the additional layers being only fibre- or fabric-reinforced layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00—Armour; Armour plates
    • F41H5/02—Plate construction
    • F41H5/04—Plate construction composed of more than one layer
    • F41H5/0471—Layered armour containing fibre- or fabric-reinforced layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2023/00—Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/04—Polymers of ethylene
    • B29K2023/06—PE, i.e. polyethylene
    • B29K2023/0658—PE, i.e. polyethylene characterised by its molecular weight
    • B29K2023/0683—UHMWPE, i.e. ultra high molecular weight polyethylene
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/25—Solid
    • B29K2105/251—Particles, powder or granules
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037—Other properties
    • B29K2995/0089—Impact strength or toughness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2007/00—Flat articles, e.g. films or sheets
    • B29L2007/007—Narrow strips, e.g. ribbons, tapes, bands
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2023/00—Tubular articles
    • B29L2023/005—Hoses, i.e. flexible
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0223—Vinyl resin fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0246—Acrylic resin fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0253—Polyolefin fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0261—Polyamide fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0276—Polyester fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/101—Glass fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/54—Yield strength; Tensile strength
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/72—Density
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2435/00—Closures, end caps, stoppers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2439/00—Containers; Receptacles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2607/00—Walls, panels
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2321/00—Fibres made from polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • D10B2321/02—Fibres made from polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds polyolefins
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2321/00—Fibres made from polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • D10B2321/06—Fibres made from polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds polymers of unsaturated alcohols, e.g. polyvinyl alcohol, or of their acetals or ketals
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2321/00—Fibres made from polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • D10B2321/10—Fibres made from polymers obtained by reactions only involving carbon-to-carbon unsaturated bonds polymers of unsaturated nitriles, e.g. polyacrylonitrile, polyvinylidene cyanide
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2331/00—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
    • D10B2331/02—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyamides
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2331/00—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products
    • D10B2331/04—Fibres made from polymers obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds, e.g. polycondensation products polyesters, e.g. polyethylene terephthalate [PET]
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2401/00—Physical properties
    • D10B2401/06—Load-responsive characteristics
    • D10B2401/062—Load-responsive characteristics stiff, shape retention
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2401/00—Physical properties
    • D10B2401/06—Load-responsive characteristics
    • D10B2401/063—Load-responsive characteristics high strength
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2505/00—Industrial
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/30—Woven fabric [i.e., woven strand or strip material]
    • Y10T442/3033—Including a strip or ribbon
    • Y10T442/3041—Woven fabric comprises strips or ribbons only

Definitions

  • the invention relates to polymeric tapes and a process for the preparation thereof and further to a material sheet comprising the polymeric tapes, and to its process of preparation.
  • the invention also relates to articles comprising the material sheet, in particular to a ballistic resistant article.
  • the invention also relates to different uses of the polymeric tapes.
  • a material sheet comprising a consolidated stack of monolayers of a unidirectionally drawn polymer is known from EP 1627719 A1.
  • This publication discloses a multilayered material sheet comprising a plurality of unidirectional monolayers consisting of ultra high molecular weight polyethylene and essentially devoid of bonding matrices, whereby the draw direction of two subsequent monolayers in the stack differs.
  • the monolayers of the multilayered material disclosed in EP 1627719 A1 are produced by positioning a plurality of tapes of ultra high molecular weight polyethylene adjacent to each other whereby adjacently positioned tapes overlap at least partly along their side edges. Without the overlap the known multilayered material cannot be produced.
  • the object of the present invention is to provide a material sheet that can be easily produced and having at least similar properties, in particular similar antiballistic properties, as the material known from EP 1627719 A1 or other commercially available materials based on unidirectional PE fibers.
  • This object is achieved according to the invention by providing a material sheet comprising a woven fabric of polymeric tapes, wherein the width of a tape varies less than 2 % on average in the longitudinal direction of the tape.
  • the polymeric tapes are tapes of a drawn polymer; more preferably, the tapes are unidirectional tapes of a drawn polymer.
  • unidirectional tapes is meant in the context of the invention tapes which show a preferred orientation of the polymer chains in one direction, i.e. in the direction of drawing.
  • Such tapes of a drawn polymer may be produced by drawing said tapes, preferably by uniaxial drawing if unidirectional tapes are to be produced and which will exhibit anisotropic mechanical properties.
  • WO2006/075961 describes a method for producing a woven material from tape-like warps and wefts comprising the steps of feeding tape- like warps to aid shed formation and fabric take-up; inserting tape-like weft in the shed formed by said warps; depositing the inserted tape-like weft at the fabric-fell; and taking-up the produced woven material; wherein said step of inserting the tape-like weft involves gripping a weft tape in an essentially flat condition by means of clamping, and pulling it through the shed.
  • the inserted weft tape is preferably cut off from its supply source at a predetermined position before being deposited at the fabric-fell position. While weft tensioning is a necessary condition for processing yarns, it is not desirable when processing tapes.
  • WO2006/075961 therefore allows to feed and process tape-like warps in a state of low tension. This is achieved by carrying out weaving in a vertical format because this way the sagging of warps and wefts due to gravity is significantly reduced.
  • the invention further relates to a polymeric tape having a width that varies less than 2% on average in the longitudinal direction of the tape.
  • said tape is a tape of a drawn polymer, more preferably, said tape is a unidirectional tape of a drawn polymer.
  • the material sheet according to the invention is readily produced.
  • the conventional material sheet as described in EP 1627719 A1 for instance, is produced by first making a monolayer of a plurality of tapes positioned adjacent to each other, and then applying another similar monolayer at an angle on top of the first monolayer.
  • adjacently positioned tapes overlap at least partly along their side edges. This process is time consuming and involves more steps than the process to make the material structure of the present invention.
  • an overlapping of the tapes is not necessary for obtaining a material sheet with at least similar properties or handling characteristic, reducing therefore the number of processing steps.
  • the tape-overlapping step can be dispensed with.
  • the material sheet of the invention is preferably produced by weaving a plurality of the unidirectional tapes of the invention with their longitudinal edges as close as possible to each other, and preferably in touching proximity. This is made possible by using unidirectional tapes having a width that varies less than 2 % on average in the longitudinal direction of the tape, as is required by the invention.
  • it would be desirable to allow a gap between adjacent tapes i.e the adjacent tapes in the material sheets are not in contact along their longitudinal edges - i.e. a gap of greater than 0%).
  • the material sheet according to the invention is characterized in that the woven sheet comprises a plurality of unidirectional tapes of the drawn polymer in the warp and weft direction, and in that the gap between adjacent tapes in the weft and/or warp direction is smaller than 10 % of the width of the adjacent unidirectional tapes, more preferably smaller than 5 % of the width of the adjacent unidirectional tapes, even more preferably smaller than 3 % of the width of the adjacent unidirectional tapes. Most preferably said gap is smaller than 1 % provided that the inventive tapes have a width variation also smaller than 1 % on average in the longitudinal direction of the tape.
  • the tapes of the invention have a width varying less than 1 % on average in the longitudinal direction of the tape. In an even further preferred embodiment the tapes have a width of at least 10 mm, more preferably at least 20 mm, most preferably at least 40 mm and further having a variation in width which is less than 1 % on average in the longitudinal direction of the tape. It was observed that a material sheet based on the tapes of this embodiment yields an even better antiballistic performance.
  • a particularly preferred embodiment of the tape according to the invention is characterized in that the polymer from which it is made is selected from the group consisting of polyolefins, polyesters, polyvinyl alcohols, polyacrylonitriles, polyamides, especially poly(p-phenylene teraphthalamide), liquid crystalline polymers and ladder-like polymers, such as polybenzimidazole or polybenzoxazole, especially - A -
  • Unidirectional tapes from these polymers are preferably highly oriented, i.e. having a crystallinity as measured by DSC of above 90%, by drawing the formed material, for instance films, at a suitable temperature.
  • An even more preferred embodiment of the tape according to the invention is characterized in that the polymer from which it is made is selected from the group consisting of polyolefins, polyesters, polyvinyl alcohols, polyacrylonitriles, and polyamides.
  • the material sheets comprising these tapes can be very well consolidated.
  • the material sheet of the invention allows the use of tapes of drawn polymers, or simply drawn tapes, with relatively low strength, and therefore does not expressly need high strength drawn tapes made of e.g. ultra high molecular weight polyethylene to obtain good antiballistic performance.
  • the tapes of the invention comprise ultra high molecular weight polyethylene.
  • the ultra high molecular weight polyethylene may be linear or branched, although preferably linear polyethylene is used.
  • Linear polyethylene is herein understood to mean polyethylene with less than 1 side chain per 100 carbon atoms, and preferably with less than 1 side chain per 300 carbon atoms; a side chain or branch generally containing at least 10 carbon atoms.
  • the linear polyethylene may further contain up to 5 mol% of one or more other alkenes that are copolymerisable therewith, such as propene, butene, pentene, 4-methylpentene, octene.
  • the linear polyethylene is of high molar mass with an intrinsic viscosity (IV, as determined on solutions in decalin at 135°C) of at least 4 dl/g; more preferably of at least 8 dl/g, most preferably of at least 10 dl/g.
  • IV intrinsic viscosity
  • Such polyethylene is also referred to as ultra high molecular weight polyethylene.
  • Intrinsic viscosity is a measure for molecular weight that can more easily be determined than actual molar mass parameters like Mn and Mw.
  • a polyethylene film of this type yields particularly good antiballistic properties.
  • the tapes according to the invention may be prepared in the form of films which is subsequently slit into tapes.
  • a preferred first process for the preparation of the tape of the invention comprises forming a polymeric powder bed, compression-moulding the polymeric powder bed at a temperature below the melting point of the polymeric powder, and preferably drawing the compression-moulded polymer, and wherein the powder bed is moulded by compression together with at least one compressible bordering means positioned onto the powder bed.
  • the invention also relates to such a process.
  • the powder bed is compression-moulded together with at least two parallel compressible bordering means, said means defining in the powder bed an in-boundary part and an out-of-boundary part or parts.
  • the melting point of the polymeric powder also called melting temperature is determined by DSC as detailed below.
  • compressible bordering means means made of a compressible material, said means partitioning the powder bed into at least two parts.
  • compressible is meant that the means do not substantially interfere with the compression moulding of the polymeric powder bed.
  • the compressible bordering means are compressible strips.
  • the undeformed strips typically only take a negligible part of the compressive pressure produced by the compression means of the compression-moulding device, preferably less than 5%, more preferably less than 2%, most preferably less than 1 %.
  • the strips act as a firm boundary for the polymeric powder and it has turned out that the use of said strips provides for a polymeric powder bed that is well controlled and of substantially uniform distribution, at least between the boundaries formed by the at least two strips.
  • the compressible bordering means and in particular the strips may be manufactured from any material that is flexible enough to provide for the desired compressibility.
  • Preferred materials include thermoplastic polymers, of which polyolefins, such as polypropylene are particularly preferred.
  • Another particularly preferred material comprises a rubber polymer, and more preferably a high temperature resistant rubber polymer, such as a silicon rubber.
  • the means, e.g. strips, are preferably made of a material having a melting temperature as determined by DSC of at least 10 0 C 1 more preferably at least 20 0 C, and most preferably at least 30 0 C higher than the melting temperature of the polymeric powder.
  • Said means, and in particular the strips may have any shape. It is possible for the means, e.g. strips, to for instance have a rectangular, triangular, circular, or polygonal cross-section, whereby the means or strips can be solid or hollow. Preferably, strips are used that are hollow since such strips are easily compressible. In a particularly preferred process according to the invention, the strips comprise a hose, or a tube.
  • the undeformed height of the means, e.g. strips can be varied within large boundaries. The undeformed height of the means, e.g. strips, is preferably equal or higher than the undeformed average thickness of the polymeric powder bed.
  • the ratio of outer diameter: inner diameter preferably is 3:2, more preferably 3:1.5 and even more preferably 3:1.
  • the compression-moulding process is carried out according to the process of US 5,091 ,133, the disclosure thereof being included herein by reference. Therefore, the invention relates to a process for the preparation of a polymeric tape, the process comprising feeding a polymeric powder between a combination of endless belts thus forming a polymeric powder bed, compression-moulding the polymeric powder bed at a temperature below the melting point of the polymeric powder, conveying the resultant compression-moulded polymer between the endless belts and preferably drawing the compression-moulded polymer, wherein at least two strips of compressible material are fed and conveyed between the endless belts together with the polymeric powder.
  • it is essential that the strips are compressible, at least in their undeformed state, by which is meant that the strips do not substantially interfere with the compression moulding of the polymeric powder bed.
  • the strips are arranged substantially parallel to each other and in the conveying direction, whereby the strips are arranged in such a way that the width of the resulting tape varies less than 2% on average in the longitudinal direction of the tape.
  • This may suitably be done by e.g. a creating a fixed distance between the strips by feeding the strips through a rack with a predefined width for the strips.
  • a rack with a predefined width for the strips.
  • two of such racks are present for best alignment of the strips, e.g. such racks are present before and after a conveying section. More preferably the strips are fed through the said rack while under tension for alignment.
  • the required tension can be easily be determined by routine experimentation, whereby too high a tension could lead to excessive deformation of the strips and too low a tension will not result in a tape with less than 2% variation of width.
  • An alternative method could be electronically controlled width-gauges between and guiding the strips.
  • the polymeric powder is fed or scattered onto the belt over some width, whereby the width is generally larger than the distance between the strips.
  • the powder bed therefore overlaps with the strips.
  • the strips are arranged such that they extend within the polymeric powder bed along the outer edges thereof, and at some distance from the outer edges.
  • the polymeric powder bed is in this way divided in a part that is in-boundary and extends between the strips, and in a part that is out-of- boundary, the latter part extending from the strips to the outer edges of the powder bed.
  • the compression-moulded out-of-boundary part(s) of the powder bed may be removed and recycled. Such process therefore offers the possibility to produce a polymeric tape substantially without waste.
  • a further particularly preferred embodiment of the process of making the tapes of the invention is characterized in that the number of strips is 2, and are used to create an in-boundary part between these 2 strips and an out-of boundary part or parts, whereby the strips are arranged such that they longitudinally extend within the polymeric powder bed along the outer edges of said bed such that the width of the out- of boundary part(s) of the powder bed does not exceed 30% of the total width of the powder bed.
  • the side regions thereof will generally show a variation in thickness, the thickness decreasing towards the sides of the powder bed. It has turned out that by positioning the strips according to this embodiment, i.e.
  • the in-boundary part of the powder bed will have a substantially uniform thickness.
  • width of the out- of-boundary parts is meant the total width of the out-of-boundary part or parts. It is believed that the more uniform thickness of the in-boundary part of the powder bed is responsible for the observed improved properties of the final polymeric tape.
  • the strips are positioned at a distance from the outer edges of the polymeric powder bed of at most 20% of the total width of the polymeric powder bed, and most preferred at a distance from the outer edges of the polymeric powder bed of at most 10% of the total width of the polymeric powder bed.
  • the polymer powder may be mixed with a suitable liquid organic compound having a boiling point higher than the melting point of said polymer.
  • Compression moulding is preferably carried out by temporarily retaining the polymer powder between the endless belts while conveying. This may for instance be done by providing pressing platens and/or rollers in connection with the endless belts.
  • the UHMWPE polymer used in this process is preferably drawable in the solid state.
  • Drawing, preferably uniaxial drawing, of the compression moulded polymer may be carried out by means known in the art. Such means comprise extrusion stretching and tensile stretching on suitable drawing units. To attain increased mechanical strength and stiffness, drawing may be carried out in multiple steps.
  • drawing is typically carried out uniaxially in a number of drawing steps.
  • the first drawing step may for instance comprise drawing to a stretch factor of 3.
  • Multiple drawing may typically result in a stretch factor of 9 for drawing temperatures up to 12O 0 C, a stretch factor of 25 for drawing temperatures up to 140 0 C, and a stretch factor of 50 for drawing temperatures up to and above 150 0 C.
  • stretch factors of about 50 and more may be reached.
  • the polymeric tape of the invention is produced by providing clear boundaries for the polymeric powder bed, e.g. in the form of the easily compressible strips, the tape is more uniform than known hitherto, in particular in the transverse direction of the tape as produced.
  • Polymeric tape of the invention may be obtained having further an areal weight varying less than 10 % on average in the transverse direction of the tape, and preferably less than 5 % on average in the transverse direction of the tape. Such more uniform tapes provide better, or at least more consistent mechanical properties than the known tapes.
  • a preferred second process for the formation of films or tapes comprises feeding a polymer to an extruder, extruding a film or a tape at a temperature above the melting point thereof and drawing the extruded film or tape.
  • the polymer prior to feeding the polymer to the extruder, the polymer may be mixed with a suitable liquid organic compound, for instance to form a gel, such as is preferably the case when using ultra high molecular weight polyethylene.
  • a suitable liquid organic compound for instance to form a gel
  • the polyethylene films are prepared by such a gel process.
  • a suitable gel spinning process is described in for example GB-A-2042414, GB-A-2051667, EP 0205960 A and WO 01/73173 A1 , and in "Advanced Fibre Spinning Technology", Ed. T. Nakajima, Woodhead Publ. Ltd (1994), ISBN 185573 182 7.
  • the gel spinning process comprises preparing a solution of a polyolefin of high intrinsic viscosity, extruding the solution into a film at a temperature above the dissolving temperature, cooling down the film below the gelling temperature, thereby at least partly gelling the film, and drawing the film before, during and/or after at least partial removal of the solvent.
  • Drawing preferably uniaxial drawing, of the produced films or tapes may be carried out by means known in the art. Such means comprise extrusion stretching and tensile stretching on suitable drawing units. To attain increased mechanical strength and stiffness, drawing may be carried out in multiple steps. In case of the preferred ultra high molecular weight polyethylene films, drawing is typically carried out uniaxially in a number of drawing steps.
  • the first drawing step may for instance comprise drawing to a stretch factor of 3. Multiple drawing may typically result in a stretch factor of 9 for drawing temperatures up to 120 c C, a stretch factor of 25 for drawing temperatures up to 140 c C, and a stretch factor of 50 for drawing temperatures up to and above 150 0 C. By multiple drawing at increasing temperatures, stretch factors of about 50 and more may be reached. This results in high strength tapes, whereby for tapes of ultra high molecular weight polyethylene, strengths of 1.5 GPa to 1.8 GPa and more may be obtained.
  • the resulting tapes may be used as such to produce the material sheet by weaving, if their variation in width is less than 2 % on average in the longitudinal direction of the tape, and preferably less than 1 % on average in the longitudinal direction of the tape.
  • the tapes and in particular the drawn tapes as produced may be cut to their desired width, or split along the direction of drawing, to obtain the limited width variation as required by the invention.
  • the material sheet is woven from tape that is not slitted e.g. to form fiber like structures as disclosed in US 5, 091 ,133.
  • the width of the tapes of the invention and in particular the width of the unidirectional tapes, is only limited by the width of the film from which they are produced.
  • the width of the tapes preferably is more than 2 mm, preferably more than 5 mm, more preferably more than 10 mm, even more preferably more than 20 mm. Most preferably the width of the tapes is more than 40 mm. It was observed that wider tapes perform better when woven into material sheets and furthermore, material sheets comprising wider tapes have further improved properties, in particular antiballistic properties, especially when the width of the tapes is more than 40 mm. In principle there is no restriction to the maximum width of the tape. For practical reasons the preferred maximum width is at most 400 mm, more preferably at most 300 mm, most preferably at most 200 mm.
  • the areal density of the tapes of the invention can be varied over a large range, for instance between 5 and 200 g/m 2 .
  • Preferred areal density is between 8 and 120 g/m 2 , more preferred between 10 and 80 g/m 2 and most preferred between 12 and 60 g/m 2 , most preferred between 12 and 30 g/m 2 .
  • the areal density of a tape can be determined by weighing a conveniently cut surface from the tape. It was observed that material sheets made of such tapes have improved antiballistic performance.
  • the thickness of the tapes of the invention can in principle be selected within wide ranges.
  • the thickness of the tapes used in weaving the material sheet of the invention does not exceed 120 ⁇ m, more preferably does not exceed 50 ⁇ m, and most preferably is comprised between 5 and 29 ⁇ m.
  • a further preferred material sheet according to the invention is characterized in that the thickness of the tapes used to manufacture thereof is greater than 10 ⁇ m and does not exceed 50 ⁇ m, preferably does not exceed 100 ⁇ m and more preferably does not exceed 120 ⁇ m.
  • the strength of the tapes of the invention largely depends on the polymer from which they are produced, and on their (uniaxial) drawing or draw ratio.
  • the strength of the tapes is at least 0.75 GPa, preferably at least 0.9 GPa, more preferably at least 1.2 GPa, even more preferably at least 1.5 GPa, even more preferably at least 1.8 GPa, and even more preferably at least 2.1 GPa, and most preferably at least 3 GPa.
  • the unidirectional tapes are preferably sufficiently interconnected to each other, meaning that the material sheets according to the invention hardly delaminate under normal use conditions such as e.g. at room temperature.
  • the material sheet according to the invention may comprise tapes woven into e.g. fabrics of any structure.
  • Suitable woven fabric structures may include plain weave, twill weave, basket weave, satin weave, crowfoot weave, and others.
  • Particularly preferred is a material sheet, wherein the woven fabric has a plain weave structure.
  • Such a structure offers a stable material sheet, which is easily processed further.
  • this embodiment shows excellent antiballistic performance, especially in a stand alone configuration.
  • Another preferred embodiment of the material sheet comprises a woven fabric having a twill weave structure.
  • Such an embodiment is preferred in ballistic resistant articles, comprising material sheets of the invention and a further sheet of inorganic material selected from the group consisting of ceramic, steel, aluminum, magnesium titanium, nickel, chromium and iron or their alloys, glass and graphite, or combinations thereof.
  • the present embodiment preferably comprises a twill weave structure with an interlacing frequency ranging from 3 - 30:1 , and more preferably ranging from 7 - 21 :1.
  • An interlacing frequency of x:1 means that a warp (or weft yarn) crosses over x weft (or warp) yarns.
  • the material sheet of the invention may also include a binder which is locally applied to bond and stabilise the plurality of the tapes, in particular unidirectional tapes used in manufacturing thereof, such that the structure of the material sheet is retained during handling and producing of structures, e.g. antiballistic structures.
  • a binder which is locally applied to bond and stabilise the plurality of the tapes, in particular unidirectional tapes used in manufacturing thereof, such that the structure of the material sheet is retained during handling and producing of structures, e.g. antiballistic structures.
  • Suitable binders are described in e.g. EP 0191306 B1 , EP 1170925 A1 , EP 0683374 B1 and EP 1144740 A1.
  • the binder may be applied in various forms and ways; for example as a transverse bonding strip (transverse with respect to the e.g. unidirectional tapes).
  • the application of the binder during the formation of the material sheet advantageously stabilises the tapes, thus enabling faster production cycles to be achieved
  • a binder is applied to fixedly abut adjacent unidirectional tapes along their longitudinal edges.
  • the role of the binder is to temporarily retain and stabilise the plurality of unidirectional tapes during handling and making of material sheets, e.g. antiballistic material sheets
  • localised application of the binder is preferred. Local application of the binder is application that is restricted to the immediate vicinity of the longitudinal edges and may include intermittent localised application (spot application along the longitudinal edges).
  • the unidirectional tapes in the weft and/or warp direction are mutually bonded, at least over an area adjacent to the longitudinal edges of the woven fabric.
  • the unidirectional tapes of the drawn polymer in the warp and weft direction of the woven fabric are at least partly adhered to each other, at least over an area adjacent to the longitudinal edges of the woven fabric by fusion bonding.
  • welding may be used for instance to intermittently fuse sections of the longitudinal edges of the material sheet together.
  • the proportion of the longitudinal edges of the material sheet comprising intermittent localised fusion is preferably less than 50%, 30%, 20% 10%, 5% or 2%.
  • the proportion of the longitudinal edges (or areas adjacent to the longitudinal edges) of the material sheet which is raised due to the application of the binder is preferably less than 50%, 30%, 20% 10%, 5% or 2%.
  • the binder comprises less than 20%, 10%, 5%, 2% 1 %, 0.5%, or 0.2% of the weight of the material sheet.
  • the material sheet according to the invention can be used in the form of one woven structure, e.g. fabric, as produced.
  • a multilayered material sheet by stacking a plurality of material sheets according to the invention (e.g. woven fabrics).
  • a multilayered material sheet preferably comprises at least 2 woven fabrics, preferably at least 4 woven fabrics, more preferably at least 6 woven fabrics, even more preferably at least 8 woven fabrics, and most preferably at least 10 woven fabrics.
  • Increasing the number of woven fabrics in the multilayer material sheet of the invention simplifies the manufacture of articles from these material sheets, for instance antiballistic plates.
  • a process for the preparation of a material sheet comprising:
  • the process is characterised in that, prior to step (c) the unidirectional tapes of the drawn polymer in the warp and weft direction of the woven fabric are at least partly adhered to each other, at least over an area adjacent to the longitudinal edges of the woven fabric, an example of which is depicted in fig. 2.
  • adhering the unidirectional tapes is performed by fusion bonding, and even more preferably by ultrasonic welding.
  • the material sheet according to the invention is particularly useful in manufacturing ballistic resistant articles, such as vests or armoured plates. Particularly good results are obtained when drawn tapes, preferably unidirectional tapes according to the invention are used in manufacturing the material sheet.
  • Ballistic applications comprise applications with ballistic threat against projectiles of several kinds including against armor piercing, so-called AP bullets and hard particles such as e.g. fragments and shrapnel.
  • the material sheet according to the invention is most suitable for use in hard ballistics, such as e.g. panels, for use in vehicles for land/air or sea, or panels for inserts in bullet resistant vests.
  • the invention therefore also relates to the enumerated ballistic resistant articles comprising the material sheet of the invention.
  • the ballistic resistant article according to the invention comprises at least 1 woven fabric layer, preferably at least 5 woven fabric layers, more preferably at least 10 woven fabric layers, even more preferably at least 15 woven fabric layers and most preferably at least 20 woven fabric layers.
  • the ballistic resistant article according to the invention comprises a further sheet of inorganic material selected from the group consisting of ceramic; metal; glass; graphite, or combinations thereof.
  • metal and in particular a metal having a melting point of at least 350 0 C, more preferably at least 500 0 C, most preferably at least 600°C.
  • Suitable metals include aluminum, magnesium, titanium, copper, nickel, chromium, beryllium, iron and copper including their alloys as e.g. steel and stainless steel and alloys of aluminum with magnesium (so-called aluminum 5000 series), and alloys of aluminum with zinc and magnesium or with zinc, magnesium and copper (so-called aluminum 7000 series). In said alloys the amount of e.g.
  • aluminum, magnesium, titanium and iron preferably is at least 50 wt%.
  • Preferred metal sheets comprising aluminum, magnesium, titanium, nickel, chromium, beryllium, iron including their alloys. More preferably the metal sheet is based on aluminum, magnesium, titanium, nickel, chromium, iron and their alloys. This results in a light antiballistic article with a good durability. Even more preferably the iron and its alloys in the metal sheet have a Brinell hardness of at least 500. Most preferably the metal sheet is based on aluminum, magnesium, titanium, and their alloys. This results in the lightest antiballistic article with the highest durability. Durability in this application means the lifetime of a composite under conditions of exposure to heat, moisture, light and UV radiation.
  • the further sheet of material may be positioned anywhere in the stack of woven fabric layers, the preferred ballistic resistant article is characterized in that the further sheet of material is positioned at the outside of the stack of woven fabric layers, most preferably at least at the strike face thereof.
  • the ballistic resistant article according to the invention preferably comprises a further sheet of the above described inorganic material having a thickness of at most 100 mm.
  • the maximum thickness of the further sheet of inorganic material is 75 mm, more preferably 50 mm, and most preferably 25 mm. This results in the best balance between weight and antiballistic properties.
  • the thickness of the metal sheet is at least 0.25 mm, more preferably at least 0.5 mm, and most preferably at least 0.75 mm. This results in even better antiballistic performance.
  • the further sheet of inorganic material may optionally be pre-treated in order to improve adhesion with the multilayer material sheet.
  • Suitable pre-treatment of the further sheet includes mechanical treatment e.g. roughening or cleaning the surface thereof by sanding or grinding, chemical etching with e.g. nitric acid and laminating with polyethylene film.
  • a bonding layer e.g. an adhesive
  • adhesive may comprise an epoxy resin, a polyester resin, a polyurethane resin or a vinylester resin.
  • the bonding layer may further comprise a woven or non woven layer of inorganic fiber, for instance glass fiber or carbon fiber. It is also possible to attach the further sheet to the multilayer material sheet by mechanical means, such as e.g. screws, bolts and snap fits.
  • the further sheet is preferably comprises a metal sheet covered with a ceramic layer.
  • ceramic layer/metal sheet/at least two unidirectional sheets with the direction of the fibers in the unidirectional sheet at an angle a to the direction of the fibers in an adjacent unidirectional sheet.
  • Suitable ceramic materials include e.g. alumina oxide, titanium oxide, silicium oxide, silicium carbide and boron carbide. The thickness of the ceramic layer depends on the level of ballistic threat but generally varies between 2 mm and 30 mm. This ballistic resistant article is preferably positioned such that the ceramic layer faces the ballistic threat.
  • a process for the manufacture of a ballistic resistant article comprising:
  • a stack of at least 2 woven fabric layers of unidirectional tapes of drawn polymer, wherein the width of a tape varies less than 2 % on average in the longitudinal direction of the tape is manufactured in a separate process, such as has been described above.
  • This pre-manufactured stack is then combined with the further sheet of material selected from the group consisting of ceramic, steel, aluminum, titanium, glass and graphite, or combinations thereof, in step (a) of the process.
  • Consolidation for all processes described above may suitably be done in a hydraulic press. Consolidation is intended to mean that the monolayers are relatively firmly attached to one another to form one unit.
  • the temperature during consolidating generally is controlled through the temperature of the press.
  • a minimum temperature generally is chosen such that a reasonable speed of consolidation is obtained.
  • 80 0 C is a suitable lower temperature limit, preferably this lower limit is at least 100 °C, more preferably at least 120 0 C, most preferably at least 140 0 C.
  • a maximum temperature is chosen below the temperature at which the drawn polymer woven layers lose their high mechanical properties due to e.g. melting.
  • the temperature is at least 10 0 C, preferably at least 15 0 C and even more at least 20 0 C below the melting temperature of the drawn polymer woven layer. In case the drawn polymer woven layer does not exhibit a clear melting temperature, the temperature at which the drawn polymer woven layer starts to lose its mechanical properties should be read instead of melting temperature.
  • a temperature below 145 0 C generally will be chosen.
  • the pressure during consolidating preferably is at least 7 MPa, more preferably at least 15 MPa, even more preferably at least 20 MPa and most preferably at least 35 MPa. In this way a stiff antiballistic article is obtained.
  • the optimum time for consolidation generally ranges from 5 to 120 minutes, depending on conditions such as temperature, pressure and part thickness and can be verified through routine experimentation. In the event that curved antiballistic articles are to be produced it may be advantageous to first pre-shape the further sheet of material into the desired shape, followed by consolidating with the monolayers and/or multilayer material sheet.
  • cooling after compression moulding at high temperature is carried out under pressure as well. Pressure is preferably maintained at least until the temperature is sufficiently low to prevent relaxation.
  • This temperature can be established by one skilled in the art.
  • typical compression temperatures range from 90 to 150 0 C, preferably from 1 15 to 130 C C.
  • Typical compression pressures range between 100 to 300 bar, preferably 100 to 180 bar, more preferably 120 to 160 bar, whereas compression times are typically between 40 to 180 minutes.
  • the multilayered material sheet and antiballistic article of the present invention are particularly advantageous over previously known antiballistic materials as they provide at least the same level of protection as the known articles at a significantly lower weight, or an improved ballistic performance at equal weight compared with the known article.
  • Starting materials are inexpensive and the manufacturing process is relatively short and thus cost effective. Since different polymers may be used to produce the multilayered material sheet of the invention properties may be optimized according to the particular application. Besides ballistic resistance, properties include for instance heat stability, shelf-life, deformation resistance, bonding capacity to other material sheets, formability, and so on.
  • the material sheet of the invention and the particular constructions comprising said sheet as described above in the embodiments of the multilayered material sheet and of the ballistic resistant articles are products particularly useful also in manufacturing cargo panels, i.e. panels used in the construction of cargo containers. Said products proved also particularly advantageous in manufacturing construction walls; liners for e.g. cargo holds such as aircraft cargo holds; cargo pallet sheets and radomes. Furthermore, said products and in particular the constructions of multilayered material sheets and ballistic resistant articles proved extremely useful when used to manufacture impact sensitive aircraft parts, e.g. wing edges, flaps or other prominent parts which are prone to suffer impacts from e.g. ice or birds.
  • the invention therefore relates to the use of the material sheet of the invention in the above enumerated products and furthermore to the above enumerated products comprising the material sheet of the invention.
  • the invention moreover relates to the use of the tapes of the invention in woven material sheets and also in a weaving process for manufacturing material sheets.
  • Fig. 1 schematically represents an embodiment of a material sheet according to the invention.
  • Fig. 2 schematically represents another embodiment of a material sheet according to the invention.
  • Fig. 3 schematically represents still another embodiment of a material sheet according to the invention.
  • Fig. 4 schematically represents a multilayer material sheet according to the invention.
  • a woven fabric of unidirectional tapes of drawn polymer is shown.
  • the width of the tapes of at least 10 mm varies less than 2 % on average in the longitudinal direction of the tapes.
  • the woven fabric has been obtained by a weaving process as described in WO2006/075961. After weaving the tapes according to a plain weave pattern (as shown in figure 1), the woven fabric is fed into a belt press or calander press, known per se, for final consolidation of the material sheet. In the belt press or calander, the unidirectional tapes running in the warp and weft direction are bonded at a temperature close to the melting point of the tapes.
  • tapes of at least 10 mm can be produced having a width varying less than 2 % on average in the longitudinal direction of the tapes by drawing polymer films.
  • a tape as produced is subsequently slitted along its longitudinal edges to obtain the limited variation in width, as required by the invention.
  • Suitable slitting equipment is for instance a Bielloni Sage machine, model Taglierina, type RP/B1 505, equipped with chromium steel knives.
  • FIG 2 another embodiment of a woven fabric of unidirectional tapes of drawn polymer is shown.
  • the width of the tapes of at least 10 mm varies less than 2 % on average in the longitudinal direction of the tapes.
  • the woven fabric has been obtained by a weaving process as described in WO2006/075961. After weaving the tapes according to a plain weave pattern, the woven fabric has been partly consolidated over an area adjacent to the longitudinal edges of the woven fabric only.
  • the dots shown in figure 2 actually represent locations in which the unidirectional tapes have been fusion bonded, for instance by welding.
  • FIG 3 still another embodiment of a woven fabric of unidirectional tapes of drawn polymer is shown.
  • the width of the tapes varies less than 2 % on average in the longitudinal direction of the tapes.
  • the woven fabric has been obtained by a weaving process as described in WO2006/075961 , and consolidated in a belt press.
  • the woven structure of this embodiment corresponds to a twill weave with an interlacing frequency of 3, i.e. a weft (warp) tape crosses over 3 warp (weft) tapes.
  • the multilayer material sheet comprises a woven fabric layer of Fig. 1 denoted as number 1 (in full lines), with below it a second woven fabric layer denoted as number 2 (in dotted lines).
  • the second woven fabric layer is positioned such that the seam lines of the respective woven fabric layers are aligned in a staggered fashion.
  • Test methods as referred to in the present application are as follows
  • Intrinsic Viscosity is determined according to method PTC-179 (Hercules Inc. Rev. Apr. 29, 1982) at 135°C in decalin, the dissolution time being 16 hours, with DBPC as anti-oxidant in an amount of 2 g/l solution, by extrapolating the viscosity as measured at different concentrations to zero concentration;
  • Tensile properties of yarn are defined and determined on multifilament yarns as specified in ASTM D885M, using a nominal gauge length of the fiber of 500 mm, a crosshead speed of 50 %/min.
  • Tensile properties of tape are defined and determined on tapes of a width of 20 mm as specified in ASTM D882, using a nominal gauge length of the tape of 440 mm, a crosshead speed of 50 mm/min.
  • Width variation of the tape is determined by measuring the largest width L and the smallest width S of a tape of a length of 20 m (or alternatively 20 tapes of a length of 1 m). The variation is L-S devided by S, expressed as percentage.
  • the melting point of a polymer is determined by DSC on a power- compensation PerkinElmer DSC-7 instrument which is calibrated with indium and tin with a heating rate of 10°C/min. For calibration (two point temperature calibration) of the DSC-7 instrument about 5 mg of indium and about 5 mg of tin are used, both weighed in at least two decimal places. Indium is used for both temperature and heat flow calibration; tin is used for temperature calibration only.
  • the furnace block of the DSC-7 is cooled with water, with a temperature of 4 0 C in order to provide a constant block temperature, for a stable baselines and good sample temperature stability.
  • the temperature of the furnace block should be stable for at least one hour before the start of the first analysis.
  • the tape is cut into small square pieces of 5mm maximum and a sample size of at least about 1 mg (+/- 0.1 mg) is taken. Typically, for a tape with a thickness of 40 micron, one square piece of 5mm is about 1 mg. For smaller thicknesses more pieces are stacked. For thicker tapes the size may be reduced, such that 1 mg sample mass is obtained at minimum.
  • the represenative sample is put into an aluminum DSC sample pan (50 ⁇ l), which is covered with an aluminum lid (round side up) and then sealed.
  • a small hole must be perforated to avoid pressure build-up (leading to pan deformation and therefore a worsening of the thermal contact).
  • a minimum of 1mg (+/- 0.1 mg) of powder is taken and charged into the sample pan.
  • the sample pan is placed in a calibrated DSC-7 instrument.
  • an empty sample pan (also covered with a pierced lid and sealed) is placed.
  • the following temperature program is run:
  • Analysis of the first heating curve is used as known in the art to determine the melting temperature of the analyzed sample.
  • the empty pan measurement is subtracted from the sample curve to correct for baseline curvature. Correction of the slope of the sample curve is performed by aligning the baseline at the flat part before and after the peaks (at 60 and 190°C for UHMWPE).
  • the peak height is the distance from the baseline to the top of the peak.
  • a ultrahigh molecular weight polyethylene powder as described in WO 93/15118 having a bulk density of 275 kg/m 3 and an active catalyst residue of 47 ppm was fed into a powder bed of a width of 30 cm. This bed was heated to a temperature of 135 0 C and pressed at a pressure of 35 bar during 1 minute.
  • the obtained tape precursor was caelered at a temperature of 140 0 C, i.e. below the melting point of the powder, and subsequently drawn to a total draw ratio of 150, to form a tape.
  • the tape as produced had a tenacity of 1.7GPa, measured on a small (20 mm) slit tape.
  • the tape had a width of about 60mm, and was slit to a width of 50.5 ⁇ 0.5 mm, using a Bielloni Sage machine, model Taglierina, type RP/B1 505, equipped with chromium steel knives. Thickness of the tape was 37 ⁇ m.
  • the tapes were converted into a woven fabric with a plain weave structure, as shown in figure 1.
  • the tape woven structure had a width of 130 cm and was stabilized by fusion at the edges of the product, as shown in figure 2. Without stabilizing the "fabric” it tends to fall apart when cutting it into ballistic panel sized sheets.
  • the woven fabric thus produced was then fed to a lamination line (manufactured by Meyer®), which is a belt press having different temperature and pressure zones.
  • the heating zone was set to a temperature of 146 0 C, followed by coaling. Pressure: 18 N/cm2. Total residence time was 2 minutes.
  • Ic - Production of armor panels from the tape Panels were made of size 50 x 50cm. A first layer of woven fabric was placed on a surface. A second layer of woven fabric was placed on top of the first layer, and in such fashion that the seam lines of the two layers were positioned in a staggered manner. The procedure was repeated until an areal density (AD) of 8 kg/m 2 was reached. The stack was then supplemented with commercially available 8 mm AL2O3 tiles (50 mm x 50 mm tiles) having a purity of at least 98%. The stack was then moved into a press and pressed at a temperature of 145 0 C and a pressure of 165 bar for 40 minutes. Cooling was performed under pressure until a temperature of 8O 0 C was reached. Total cycle time was about 70 minutes. Id - Performance testing of armored panels
  • V50 is the speed at which 50% of the projectiles will penetrate the armoured plate.
  • the testing procedure was as follows. The first projectile was fired at the anticipated V50 speed. The actual speed was measured shortly before impact. If the projectile was stopped, a next projectile was fired at an intended speed of about 20 m/s higher. If it perforated, the next projectile was fires at an intended speed of about 20 m/s lower. The actual speed of impact was always measured. V50 was the average of the two highest stops and the two lowest perforations.
  • the ballistic article of the present invention produced a significantly higher V50 value than is known from the prior art.

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Ceramic Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Woven Fabrics (AREA)
  • Laminated Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Compositions Of Macromolecular Compounds (AREA)

Abstract

L'invention porte sur une feuille de matériau, comprenant un tissu tissé de bandes de polymère, la largeur d'une bande variant de moins de 2 % en moyenne dans la direction longitudinale de la bande. L'invention porte également sur un procédé pour la préparation de la feuille de matériau, et sur un article résistant aux projectiles comprenant la feuille de matériau. Un article résistant aux projectiles comprenant la feuille de matériau présente d'excellentes propriétés de résistance aux projectiles.
PCT/EP2008/009122 2007-10-31 2008-10-29 Feuille de matériau et procédé pour sa préparation WO2009056287A1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US12/740,475 US20110174147A1 (en) 2007-10-31 2008-10-29 Material sheet and process for its preparation
EP20080829955 EP2205927B1 (fr) 2007-10-31 2008-10-29 Procédé pour la préparation de bande en matériau polymère
KR1020167002867A KR101647940B1 (ko) 2007-10-31 2008-10-29 재료 쉬트 및 그의 제조 방법
AU2008317960A AU2008317960B2 (en) 2007-10-31 2008-10-29 Material sheet and process for its preparation
CN200880114233.7A CN101842658B (zh) 2007-10-31 2008-10-29 材料板及其制造方法
IL204659A IL204659A (en) 2007-10-31 2010-03-22 Sheet of material and process for preparation
US14/977,046 US20160107344A1 (en) 2007-10-31 2015-12-21 Material sheet and process for its preparation
US16/248,668 US10632652B2 (en) 2007-10-31 2019-01-15 Material sheet and process for its preparation

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
US109607P 2007-10-31 2007-10-31
EP07021267 2007-10-31
EP07021267.5 2007-10-31
US61/001,096 2007-10-31
EP08001815 2008-01-31
EP08001815.3 2008-01-31

Related Child Applications (2)

Application Number Title Priority Date Filing Date
US12/740,475 A-371-Of-International US20110174147A1 (en) 2007-10-31 2008-10-29 Material sheet and process for its preparation
US14/977,046 Division US20160107344A1 (en) 2007-10-31 2015-12-21 Material sheet and process for its preparation

Publications (1)

Publication Number Publication Date
WO2009056287A1 true WO2009056287A1 (fr) 2009-05-07

Family

ID=40351342

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2008/009122 WO2009056287A1 (fr) 2007-10-31 2008-10-29 Feuille de matériau et procédé pour sa préparation

Country Status (7)

Country Link
US (3) US20110174147A1 (fr)
EP (2) EP2693158B1 (fr)
KR (2) KR101647940B1 (fr)
CN (1) CN101842658B (fr)
AU (1) AU2008317960B2 (fr)
IL (1) IL204659A (fr)
WO (1) WO2009056287A1 (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009133060A1 (fr) * 2008-04-28 2009-11-05 Teijin Aramid B.V. Articles résistant aux balles comprenant des bandes
WO2014135805A1 (fr) * 2013-03-08 2014-09-12 Hexcel Reinforcements Tissu notamment de fils de carbone présentant une faible variabilité d'épaisseur combinée à une gamme spécifique de masse surfacique
CN104838226A (zh) * 2012-12-06 2015-08-12 纱帝公司 弹道防护纺织结构及其制造方法
WO2017021143A1 (fr) * 2015-07-31 2017-02-09 Teijin Aramid Gmbh Panneau blindé
US10012478B2 (en) 2012-07-27 2018-07-03 Np Aerospace Limited Armour
US11041697B2 (en) 2014-10-31 2021-06-22 Hardwire, Llc Soft ballistic resistant armor

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006129632A1 (fr) * 2005-05-30 2006-12-07 Kaneka Corporation Procede de fabrication d'un film de graphite et film de graphite obtenu par ce procede
US20090217811A1 (en) 2006-01-17 2009-09-03 David William Leeming Textile armour
US7964267B1 (en) * 2007-04-13 2011-06-21 Bae Systems Tensylon H.P.M., Inc. Ballistic-resistant panel including high modulus ultra high molecular weight polyethylene tape
US20110180279A1 (en) * 2010-01-24 2011-07-28 Lehavot Fire Protection Ltd. Device and method of protecting a fire extinguisher
US9243354B2 (en) 2013-03-15 2016-01-26 Honeywell International Inc. Stab and ballistic resistant articles
US10443160B2 (en) 2013-03-15 2019-10-15 Honeywell International Inc. Breathable light weight unidirectional laminates
US9243355B2 (en) 2013-03-15 2016-01-26 Honeywell International Inc. Ballistic resistant thermoplastic sheet, process of making and its applications
CN104964606B (zh) * 2015-05-12 2016-12-07 郑州中远防务材料有限公司 织物及其制备方法、防护制品
ES2822933T3 (es) * 2016-11-04 2021-05-05 Airbus Operations Sl Estructura de panel para una aeronave y procedimiento de fabricación de la misma
EP4208487A1 (fr) * 2020-09-03 2023-07-12 SABIC Global Technologies B.V. Polymères polyéthylène de masse moléculaire ultra élevée présentant une morphologie et une aptitude au traitement améliorées
KR102306875B1 (ko) * 2020-12-07 2021-09-28 코오롱플라스틱 주식회사 직물형태의 복합소재 시트 제조방법과 제조장치 및 그에 의해 제조된 직물형태의 복합소재 시트

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4290248A (en) * 1975-01-06 1981-09-22 William James Kemerer Continuous process for forming products from thermoplastic polymeric material having three-dimensional patterns and surface textures
GB1601760A (en) * 1977-05-16 1981-11-04 Carpenter Technology Corp Shaped articles and powder metallurgy and method of making the same
EP0269151A1 (fr) 1986-10-31 1988-06-01 Dyneema V.O.F. Procédé pour la fabrication d'articles en polyéthylène présentant une résistance à la traction et un module d'élasticité élevé et un bon comportement au fluage, et produits obtenus par ce procédé
US5091133A (en) 1988-12-21 1992-02-25 Nippon Oil Co., Ltd. Continuous production process of high-strength and high-modulus polyolefin material
WO1993015118A1 (fr) 1992-01-28 1993-08-05 Dsm N.V. POLYMERE D'ETHYLENE A VISCOSITE INTRINSEQUE D'AU MOINS 4 dl/g ET SON PROCEDE DE PREPARATION
JPH0610233A (ja) * 1991-10-30 1994-01-18 San Retsukusu Kogyo Kk 超高分子量ポリエチレン織布及び製造方法
US6450208B1 (en) 1997-04-14 2002-09-17 Tape Weaving Sweden Ab Woven material comprising tape-like warp and weft and an aid for producing the same
WO2003008190A1 (fr) * 2001-07-19 2003-01-30 Lankhorst Indutech B.V. Film, bande ou fil de polyolefine
WO2006002977A1 (fr) * 2004-07-02 2006-01-12 Dsm Ip Assets B.V. Ensemble souple a resistance balistique
EP1627719A1 (fr) 2004-08-16 2006-02-22 FMS Enterprises Migun Ltd. Matériau multicouche à base de polyéthylène et article de protection ballistique fabriqué à partir de ce matériau.
WO2006075961A1 (fr) 2005-01-17 2006-07-20 Tape Weaving Sweden Ab Procede et appareil de tissage de chaine et de trame en forme de bande et materiau ainsi realise
WO2007003334A1 (fr) * 2005-06-30 2007-01-11 Dsm Ip Assets B.V. Article pare-balles

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2867845A (en) * 1956-11-28 1959-01-13 Us Rubber Co Apparatus for molding and curing belts
US4165960A (en) * 1976-11-24 1979-08-28 Lemelson Jerome H Continuous molding apparatus
NL177840C (nl) 1979-02-08 1989-10-16 Stamicarbon Werkwijze voor het vervaardigen van een polyetheendraad.
NL177759B (nl) 1979-06-27 1985-06-17 Stamicarbon Werkwijze ter vervaardiging van een polyetheendraad, en de aldus verkregen polyetheendraad.
US4623574A (en) 1985-01-14 1986-11-18 Allied Corporation Ballistic-resistant composite article
DE3675079D1 (de) 1985-06-17 1990-11-29 Allied Signal Inc Polyolefinfaser mit hoher festigkeit, niedrigem schrumpfen, ultrahohem modul, sehr niedrigem kriechen und mit guter festigkeitserhaltung bei hoher temperatur sowie verfahren zu deren herstellung.
US4708839A (en) 1985-12-30 1987-11-24 Amphenol Corporation Method of compressively molding articles from resin coated filler materials
US4868040A (en) * 1988-10-20 1989-09-19 Canadian Patents & Development Limited Antiballistic composite armor
US5578373A (en) * 1990-11-01 1996-11-26 Nippon Oil Co., Ltd. Split polyethylene stretched material and process for producing the same
JP3609107B2 (ja) * 1992-11-20 2005-01-12 インターメタリックス株式会社 圧粉成形体成形方法及び装置
US5619748A (en) * 1993-04-07 1997-04-15 Safariland Ltd., Inc. Ballistic vest
US5437905A (en) 1994-05-17 1995-08-01 Park; Andrew D. Ballistic laminate structure in sheet form
US6107220A (en) * 1996-10-18 2000-08-22 E. I. Du Pont De Nemours And Company Rapid fabric forming
US6010141A (en) 1997-08-06 2000-01-04 Global Polymer Industries, Inc. Molded bearing plate assembly
US6119575A (en) * 1998-02-17 2000-09-19 American Body Armor Body armor
CA2359965C (fr) 1999-01-18 2006-07-25 Twaron Products Gmbh Materiau resistant a la penetration comprenant un tissu ayant un rapport de forte densite lineaire entre deux jeux de fils
US6448359B1 (en) 2000-03-27 2002-09-10 Honeywell International Inc. High tenacity, high modulus filament
IL144100A (en) 2000-07-06 2006-08-01 Samsung Electronics Co Ltd A method based on MAC address in communication restriction
US6951685B1 (en) * 2001-11-27 2005-10-04 Integrated Textile Systems, Inc. Ultra high molecular weight polyethylene fibers

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4290248A (en) * 1975-01-06 1981-09-22 William James Kemerer Continuous process for forming products from thermoplastic polymeric material having three-dimensional patterns and surface textures
GB1601760A (en) * 1977-05-16 1981-11-04 Carpenter Technology Corp Shaped articles and powder metallurgy and method of making the same
EP0269151A1 (fr) 1986-10-31 1988-06-01 Dyneema V.O.F. Procédé pour la fabrication d'articles en polyéthylène présentant une résistance à la traction et un module d'élasticité élevé et un bon comportement au fluage, et produits obtenus par ce procédé
US5091133A (en) 1988-12-21 1992-02-25 Nippon Oil Co., Ltd. Continuous production process of high-strength and high-modulus polyolefin material
JPH0610233A (ja) * 1991-10-30 1994-01-18 San Retsukusu Kogyo Kk 超高分子量ポリエチレン織布及び製造方法
WO1993015118A1 (fr) 1992-01-28 1993-08-05 Dsm N.V. POLYMERE D'ETHYLENE A VISCOSITE INTRINSEQUE D'AU MOINS 4 dl/g ET SON PROCEDE DE PREPARATION
US6450208B1 (en) 1997-04-14 2002-09-17 Tape Weaving Sweden Ab Woven material comprising tape-like warp and weft and an aid for producing the same
WO2003008190A1 (fr) * 2001-07-19 2003-01-30 Lankhorst Indutech B.V. Film, bande ou fil de polyolefine
WO2006002977A1 (fr) * 2004-07-02 2006-01-12 Dsm Ip Assets B.V. Ensemble souple a resistance balistique
EP1627719A1 (fr) 2004-08-16 2006-02-22 FMS Enterprises Migun Ltd. Matériau multicouche à base de polyéthylène et article de protection ballistique fabriqué à partir de ce matériau.
WO2006075961A1 (fr) 2005-01-17 2006-07-20 Tape Weaving Sweden Ab Procede et appareil de tissage de chaine et de trame en forme de bande et materiau ainsi realise
WO2007003334A1 (fr) * 2005-06-30 2007-01-11 Dsm Ip Assets B.V. Article pare-balles

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
HERCULES INC. REV., 29 April 1982 (1982-04-29)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009133060A1 (fr) * 2008-04-28 2009-11-05 Teijin Aramid B.V. Articles résistant aux balles comprenant des bandes
US10012478B2 (en) 2012-07-27 2018-07-03 Np Aerospace Limited Armour
CN104838226A (zh) * 2012-12-06 2015-08-12 纱帝公司 弹道防护纺织结构及其制造方法
WO2014135805A1 (fr) * 2013-03-08 2014-09-12 Hexcel Reinforcements Tissu notamment de fils de carbone présentant une faible variabilité d'épaisseur combinée à une gamme spécifique de masse surfacique
FR3002954A1 (fr) * 2013-03-08 2014-09-12 Hexcel Reinforcements Procede et machine d'etalement d'une nappe textile de type tissu et tissus obtenus
US9637850B2 (en) 2013-03-08 2017-05-02 Hexcel Reinforcements Method and machine for spreading a fabric-type textile sheet
US11041697B2 (en) 2014-10-31 2021-06-22 Hardwire, Llc Soft ballistic resistant armor
WO2017021143A1 (fr) * 2015-07-31 2017-02-09 Teijin Aramid Gmbh Panneau blindé

Also Published As

Publication number Publication date
CN101842658A (zh) 2010-09-22
EP2205927B1 (fr) 2015-04-01
KR20160018865A (ko) 2016-02-17
IL204659A (en) 2016-07-31
US20160107344A1 (en) 2016-04-21
US10632652B2 (en) 2020-04-28
IL204659A0 (en) 2010-11-30
KR101647940B1 (ko) 2016-08-11
AU2008317960B2 (en) 2014-07-10
EP2693158B1 (fr) 2017-12-13
AU2008317960A1 (en) 2009-05-07
CN101842658B (zh) 2016-04-13
EP2205927A1 (fr) 2010-07-14
EP2693158A1 (fr) 2014-02-05
US20110174147A1 (en) 2011-07-21
KR20100087307A (ko) 2010-08-04
US20190152098A1 (en) 2019-05-23

Similar Documents

Publication Publication Date Title
US10632652B2 (en) Material sheet and process for its preparation
US9863742B2 (en) Multilayered material sheet and process for its preparation
US9625237B2 (en) Mutilayered material sheet and process for its preparation
EP2679947A1 (fr) Pile de premières et secondes couches, panneau et objet pare-balles comprenant la pile ou le panneau
CA2820423C (fr) Bande et produits la contenant
KR101485309B1 (ko) 다층 재료 시트 및 이의 제조 방법

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 200880114233.7

Country of ref document: CN

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 08829955

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 204659

Country of ref document: IL

WWE Wipo information: entry into national phase

Ref document number: 2008829955

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2204/DELNP/2010

Country of ref document: IN

WWE Wipo information: entry into national phase

Ref document number: 2008317960

Country of ref document: AU

ENP Entry into the national phase

Ref document number: 2008317960

Country of ref document: AU

Date of ref document: 20081029

Kind code of ref document: A

Ref document number: 20107009534

Country of ref document: KR

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 12740475

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE